The correctness and feasibility for using the method in trajectory calculating are proved through calculation of the maximum permissible launch ranges of the air to ground missile launch envelops. 本文通过对某空地导弹发射包线中的最大允许发射距离的实例计算,证明了应用模糊推理合成法处理弹道问题的正确性与可行性。
In this paper, the structural static analysis of the combination of the wing and the cabin of a type of air to ground missile was carried out by using the compostie material structural stress analysis software ( CMSSA ). 本文利用自行开发的复合材料结构应力分析软件(CMSSA)对某型导弹的复合材料弹翼&弹身组合结构进行了静力分析。
Study on the Trajectory Characteristic of Minimum Launch Range for Air to Ground Missile 空地导弹最小射程弹道特性研究
The results of the study have shown that the minimum launch range for air to ground missile is effected by the moment of control after launch, the speed of aircraft, the launch altitude, the difference of altitude during glide flight and so. 研究结果表明,空地导弹的最小射程由启控时机、载机初速、投放高度、下滑高度差及末制导最小距离等因素决定。
Study on the Lethality and of Air - to - Ground Missile Air(初三适用)侵彻型空地导弹的杀伤威力研究